Designs and methods are provided for an energy attenuating device. In one exemplary embodiment the device comprises an elongated metal tube having an expanded portion at a first end thereof, and an unexpanded portion extending from the expanded portion to a second end, wherein the first end is attached to a fixed structure. A mandrel is disposed in the expanded portion of the elongated metal tube, having a diameter greater than the inside diameter of the unexpanded portion of the metal tube. A tension member is attached to the mandrel and extends out of the second end of the metal tube.
|
1. An energy attenuating seating system for use in a vehicle compartment, comprising:
a generally horizontal seat platform adapted for vertical motion relative to the vehicle compartment;
an energy attenuating device comprising a metal tube held fixed at one end, and an oversized mandrel disposed in the tube;
a cable attached to the mandrel and extending out the other end of the metal tube, the cable supporting the seat platform in a vertical direction, wherein the front end of the seat platform is pivotally mounted to a rigid seat frame, and the cable extends from the energy attenuating device, around a pulley attached to a back end of the seat platform, and through a one-way clutch device.
8. A method of attenuating the force imparted to a seated passenger in a vehicle when the vehicle is exposed to an explosive energy pulse, comprising:
providing a metal tube with an expanded portion at one end, and an unexpanded portion extending from the expanded portion to the other end;
attaching the expanded portion end of the metal tube to a rigid seat frame;
attaching a first end of a cable to an oversized mandrel disposed in the expanded portion of the tube;
extending the cable out through the other end of the metal tube;
fixing a distal portion of the cable substantially beyond the other end of the metal tube to the rigid seat frame;
supporting a moveable bottom part of the seat with a portion of the cable between the first end and the fixed distal portion;
pivotally attaching a front of the seat bottom to the rigid seat frame;
mounting the metal tube under the seat bottom with the expanded end thereof also pivotally attached to the rigid seat frame; and
extending the portion of the cable between the first end and the fixed distal portion around a pulley attached to the back end of the seat bottom, wherein the distal portion of the cable is fixed to a seat back portion of the rigid seat frame substantially above the pulley.
2. The energy attenuating seating system of
3. The energy attenuating seating system of
4. The energy attenuating seating system of
5. The energy attenuating seating system of
6. The energy attenuating seating system of
7. The energy attenuating seating system of
9. The method of
10. The method of
|
Provisional Patent Application Ser. No. 61/604,389, to which the present application claims priority, is hereby incorporated by reference. The field of the present disclosure relates generally to energy attenuating (“EA”) devices for absorbing or attenuating high energy shock loads. The field may further relate to use of EA devices in vehicles, and more particularly minimizing injury to vehicle crew members during an under vehicle mine blast or other potentially lethal, sudden impact event.
In the accompanying drawings:
The instant invention is described more fully hereinafter with reference to the accompanying drawings and/or photographs, in which one or more exemplary embodiments of the invention are shown. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be operative, enabling, and complete. Accordingly, the particular arrangements disclosed are meant to be illustrative only and not limiting as to the scope of the invention. Moreover, many embodiments, such as adaptations, variations, modifications, and equivalent arrangements, will be implicitly disclosed by the embodiments described herein and fall within the scope of the present invention.
Although specific terms are employed herein, they are used in a generic and descriptive sense only and not for purposes of limitation. Unless otherwise expressly defined herein, such terms are intended to be given their broad ordinary and customary meaning not inconsistent with that applicable in the relevant industry and without restriction to any specific embodiment hereinafter described. As used herein, the article “a” is intended to include one or more items. Where only one item is intended, the term “one”, “single”, or similar language is used. When used herein to join a list of items, the term “or” denotes at least one of the items, but does not exclude a plurality of items of the list.
For exemplary methods or processes of the invention, the sequence and/or arrangement of steps described herein are illustrative and not restrictive. Accordingly, it should be understood that, although steps of various processes or methods may be shown and described as being in a sequence or temporal arrangement, the steps of any such processes or methods are not limited to being carried out in any particular sequence or arrangement, absent an indication otherwise. Indeed, the steps in such processes or methods generally may be carried out in various different sequences and arrangements while still falling within the scope of the present invention.
Additionally, any references to advantages, benefits, unexpected results, or operability of the present invention are not intended as an affirmation that the invention has been previously reduced to practice or that any testing has been performed. Likewise, unless stated otherwise, use of verbs in the past tense (present perfect or preterit) is not intended to indicate or imply that the invention has been previously reduced to practice or that any testing has been performed.
Referring now specifically to the drawings, a tube-expansion energy attenuation (EA) device according to one exemplary embodiment of the present disclosure is illustrated in
Referring to
In operation, a pulling force is applied to the end of cable 8 in the direction indicated by arrow ‘F’ in
However, if the downward load applied by the seat 22 to EA device 1 exceeds a certain threshold value, such as may occur for example during an under vehicle mine blast, the seat and the tube portion of EA device 1 will begin to move downward relative to cable 28 and the mandrel portion of the device. As the seat moves downward, the mandrel spreads the tube portion of EA device 1, absorbing energy. The seat will continue moving downward until the EA device 1 absorbs all of the energy of the event, or until the seat mechanically bottoms out against some other structure, whichever occurs first.
Clutch device 46 operates like a cable ascender, allowing the cable to be pulled through in one direction but not the other direction. In particular, the device is configured to unlock and allow cable 38 to be pulled through it in an upward direction, but locks and prevents the cable from moving when the cable is pulled in a downward direction. Thus clutch device 46 prevents the second side of cable 38 from being pulled downward; and under normal, non-EA event conditions, the EA device 1 prevents the first side of cable 38 from being pulled downward. Accordingly the back of seat 32 is fully supported by cable 38 via pulley 40, and unable to move downward under non-EA event conditions.
However, during an EA type of event, if the downward load applied by the seat 32 and pulley 40 to the cable 38 exceeds a certain threshold value, the mandrel portion of EA device 1 will begin to move downward in the tube portion of the device. The downward motion of one side of the cable 38 consequently allows the back of the seat to move downward as the front of the seat pivots about joint 36. The seat will continue pivoting downward with the EA device absorbing energy until the load on the seat drops below the threshold value, or the seat mechanically bottoms out, whichever occurs first. The seat will then automatically reset when the load on the seat is reduced further to a reset load value. The seat reset value may be any load between zero, and the threshold value, including a load value on the order of the static weight of a seated occupant.
More specifically, when the seat load goes below the reset load value, tension spring 44 will pull the second side of the cable 38 upward through clutch device 46, taking up the slack and pulling the seat back up to the starting position of
When cable 38 is placed in tension from a seat load, clutch device 46 prevents the cable from moving, and the back of the seat is thus supported by the cable and pulley 40. If the seat load reaches a point at which the downward load on pulley 40 exceeds the threshold value for the EA device, the mandrel portion of EA device will begin to displace downward along with pulley 40. The downward motion of pulley 40 consequently allows the back of the seat to move downward as the front of the seat pivots about joint 36. In this embodiment the downward motion of the seat is at exactly twice the rate of the downward motion of pulley 40. After the EA event, the seat resets itself by spring 44 pulling the cable 48 downward through clutch device 46, and the seat back up to the starting position of
Another embodiment of an exemplary, resettable, tube-expansion EA seating system is illustrated in
Referring particularly to
As best seen in
However, when the tension in cable 58 exceeds the threshold value, such as during a high energy vertical impact event, mandrel 61 will displace, expanding the tube portion of the EA devices, and allowing the back of the seat to move downward. As in the previous embodiments the seat will continue moving until the seat load being transmitted to cables 58 drops below the threshold value, or until the seat mechanically bottoms out, whichever occurs first. After the EA event, the spring loaded take-up reels 64 pull the cables 58 upward through clutch devices 46, bringing the seat up with it. The EA seat system is then reset and ready for another EA event, again as long as there is sufficient stroke remaining in the EA device.
For the purposes of describing and defining the present invention it is noted that the use of relative terms, such as “substantially”, “generally”, “approximately”, and the like, are utilized herein to represent an inherent degree of uncertainty that may be attributed to any quantitative comparison, value, measurement, or other representation. These terms are also utilized herein to represent the degree by which a quantitative representation may vary from a stated reference without resulting in a change in the basic function of the subject matter at issue.
Exemplary embodiments of the present invention are described above. No element, act, or instruction used in this description should be construed as important, necessary, critical, or essential to the invention unless explicitly described as such. Although only a few of the exemplary embodiments have been described in detail herein, those skilled in the art will readily appreciate that many modifications are possible in these exemplary embodiments without materially departing from the novel teachings and advantages of this invention. Accordingly, all such modifications are intended to be included within the scope of this invention as defined in the appended claims.
In the claims, any means-plus-function clauses are intended to cover the structures described herein as performing the recited function and not only structural equivalents, but also equivalent structures. Thus, although a nail and a screw may not be structural equivalents in that a nail employs a cylindrical surface to secure wooden parts together, whereas a screw employs a helical surface, in the environment of fastening wooden parts, a nail and a screw may be equivalent structures. Unless the exact language “means for” (performing a particular function or step) is recited in the claims, a construction under §112, 6th paragraph is not intended. Additionally, it is not intended that the scope of patent protection afforded the present invention be defined by reading into any claim a limitation found herein that does not explicitly appear in the claim itself.
Wilhelm, Terry, Bosen, David A., Larson, Ryan Michael
Patent | Priority | Assignee | Title |
10480908, | Feb 04 2015 | ST ENGINEERING LAND SYSTEMS LTD | Energy absorption system and device |
10814750, | Sep 07 2015 | NINGBO GEELY AUTOMOBILE RESEARCH & DEVELOPMENT CO , LTD | Method and vehicle seat arrangement comprising a deformation portion |
11597301, | May 04 2018 | ARMORWORKS ENTERPRISES, INC | Weight sensing energy attenuator |
Patent | Priority | Assignee | Title |
3143321, | |||
4523730, | Nov 02 1981 | Engineering Patents and Equipment Limited | Energy-absorbing seat arrangement |
4997233, | Apr 05 1988 | Israel Aircraft Industries, Ltd. | Integrated energy attentuating vehicle passenger seat |
5351791, | May 18 1990 | Device and method for absorbing impact energy | |
6308809, | May 07 1999 | Safety By Design Company | Crash attenuation system |
6457570, | May 07 1999 | Safety By Design Company | Rectangular bursting energy absorber |
6695065, | Jun 19 2001 | WEATHERFORD TECHNOLOGY HOLDINGS, LLC | Tubing expansion |
8408643, | Sep 30 2009 | Airbus Helicopters | Seat for powered aircraft, the seat incorporating means for protecting its passenger in the event of a crash |
8616635, | Feb 23 2010 | Airbus Helicopters | Anti-crash seat for a vehicle |
8702147, | Mar 11 2009 | The Penn State Research Foundation | Dual stage variable load energy absorber for vehicle seating |
20100270836, |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Feb 27 2013 | Armorworks Enterprises LLC | (assignment on the face of the patent) | / | |||
Jun 12 2013 | LARSON, RYAN MICHAEL | Armorworks Enterprises, LLC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 032236 | /0857 | |
Jun 17 2013 | WILHELM, TERRY | Armorworks Enterprises, LLC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 032236 | /0857 | |
Jun 21 2013 | BOSEN, DAVID A | Armorworks Enterprises, LLC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 032236 | /0857 | |
Jun 30 2017 | ARMORWORKS ENTERPRISES, INC | THE PRIVATEBANK AND TRUST COMPANY | SECURITY INTEREST SEE DOCUMENT FOR DETAILS | 043830 | /0237 | |
Mar 12 2024 | ARMORWORKS ENTERPRISES, INC | UMPQUA BANK | SECURITY INTEREST SEE DOCUMENT FOR DETAILS | 067398 | /0330 |
Date | Maintenance Fee Events |
May 14 2018 | BIG: Entity status set to Undiscounted (note the period is included in the code). |
May 14 2018 | M1551: Payment of Maintenance Fee, 4th Year, Large Entity. |
Jul 11 2022 | REM: Maintenance Fee Reminder Mailed. |
Oct 21 2022 | M1552: Payment of Maintenance Fee, 8th Year, Large Entity. |
Oct 21 2022 | M1555: 7.5 yr surcharge - late pmt w/in 6 mo, Large Entity. |
Date | Maintenance Schedule |
Nov 18 2017 | 4 years fee payment window open |
May 18 2018 | 6 months grace period start (w surcharge) |
Nov 18 2018 | patent expiry (for year 4) |
Nov 18 2020 | 2 years to revive unintentionally abandoned end. (for year 4) |
Nov 18 2021 | 8 years fee payment window open |
May 18 2022 | 6 months grace period start (w surcharge) |
Nov 18 2022 | patent expiry (for year 8) |
Nov 18 2024 | 2 years to revive unintentionally abandoned end. (for year 8) |
Nov 18 2025 | 12 years fee payment window open |
May 18 2026 | 6 months grace period start (w surcharge) |
Nov 18 2026 | patent expiry (for year 12) |
Nov 18 2028 | 2 years to revive unintentionally abandoned end. (for year 12) |